A standard spacecraft bus compatible with NASA launch vehicles, including STS, for four reference missions (Sun, Earth, stellar pointing from low Earth orbit, Earth pointing from geostationary orbit) was designed. The modular serviceable design stems from its use of passive acme screws for module attachment and scoop proof electrical connectors for electrical interfaces. A flight support system includes command and telemetry links.
Multimission Modular Spacecraft (MMS). A Serviceable Design Spacecraft
1987
4 pages
Report
Keine Angabe
Englisch
Multimission modular spacecraft (MMS)
NTRS | 1988
|Multimission modular spacecraft (MMS)
AIAA | 1988
|Design objectives of the multimission modular spacecraft
NTRS | 1982
|Multimission spacecraft dataplexer
Tema Archiv | 1975
|Testing programs for the Multimission Modular Spacecraft
NTRS | 1978
|